RU2015143679A - TURBINE RING FOR A TURBO MACHINE - Google Patents

TURBINE RING FOR A TURBO MACHINE Download PDF

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Publication number
RU2015143679A
RU2015143679A RU2015143679A RU2015143679A RU2015143679A RU 2015143679 A RU2015143679 A RU 2015143679A RU 2015143679 A RU2015143679 A RU 2015143679A RU 2015143679 A RU2015143679 A RU 2015143679A RU 2015143679 A RU2015143679 A RU 2015143679A
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RU
Russia
Prior art keywords
sector
support
damping device
hook
ring according
Prior art date
Application number
RU2015143679A
Other languages
Russian (ru)
Other versions
RU2015143679A3 (en
RU2653710C2 (en
Inventor
Кароль ЖОРЕГИБЕРРИ
Манюэль СИЛЬВА
Original Assignee
Турбомека
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Турбомека filed Critical Турбомека
Publication of RU2015143679A publication Critical patent/RU2015143679A/en
Publication of RU2015143679A3 publication Critical patent/RU2015143679A3/ru
Application granted granted Critical
Publication of RU2653710C2 publication Critical patent/RU2653710C2/en

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/11—Shroud seal segments
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/40—Use of a multiplicity of similar components

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Aviation & Aerospace Engineering (AREA)

Claims (14)

1. Кольцо турбины, содержащее:1. A turbine ring containing: по существу цилиндрическую опору (31); и, по меньшей мере,a substantially cylindrical support (31); and at least один сектор (32), образующий окружность, выполненную с возможностью определять сегмент воздушного канала, при этом каждый сектор (32) прикреплен к опоре (31) крепежным устройством (33a, 33b);one sector (32) forming a circle configured to define a segment of the air channel, with each sector (32) attached to the support (31) by a mounting device (33a, 33b); в котором крепежное устройство (33a) содержит участок (35) крюка, принадлежащий опоре (31) и выступающий в направлении сектора (32), и участок (34) крюка, принадлежащий сектору (32) и выступающий в направлении опоры (31), при этом участки крюка опоры и сектора (34, 35) выполнены с возможностью взаимодействия для крепления сектора (32) к опоре (31);wherein the fixing device (33a) comprises a hook portion (35) belonging to the support (31) and protruding in the direction of the sector (32), and a hook portion (34) belonging to the sector (32) and protruding in the direction of the support (31), when this, the hook sections of the support and the sector (34, 35) are made with the possibility of interaction for mounting the sector (32) to the support (31); отличающееся тем, что кольцо содержит демпфирующее устройство (50), расположенное внутри крепежного устройства (33a) и нагруженное в радиальном направлении между участком (34e) сектора и участком (31i) опоры с возможностью демпфирования относительных перемещений между сектором (32) и опорой (31); причем демпфирующее устройство (56) находится в контакте поочередно, в направлении окружности, с внутренней поверхностью опоры (31) и с внешней поверхностью участка крюка сектора (32).characterized in that the ring comprises a damping device (50) located inside the fastening device (33a) and radially loaded between the sector section (34e) and the support section (31i) with the possibility of damping relative movements between the sector (32) and the support (31 ); moreover, the damping device (56) is in contact alternately in the circumferential direction with the inner surface of the support (31) and with the outer surface of the hook section of the sector (32). 2. Кольцо по п. 1, отличающееся тем, что демпфирующее устройство содержит гибкую полосу (50), предпочтительно элемент, изготовленный из листового металла.2. The ring according to claim 1, characterized in that the damping device comprises a flexible strip (50), preferably an element made of sheet metal. 3. Кольцо по п. 1, отличающееся тем, что демпфирующее устройство (50) нагружено в радиальном направлении между участком (34e) сектора и участком (31i) опоры по всей его длине.3. The ring according to claim 1, characterized in that the damping device (50) is radially loaded between the sector portion (34e) and the bearing portion (31i) along its entire length. 4. Кольцо по п. 1, отличающееся тем, что демпфирующее устройство (50) расположено между внешней поверхностью (34e) участка (34) крюка сектора (32) и внутренней поверхностью (31i) опоры (31).4. The ring according to claim 1, characterized in that the damping device (50) is located between the outer surface (34e) of the sector (34) of the sector hook (32) and the inner surface (31i) of the support (31). 5. Кольцо по п. 1, отличающееся тем, что демпфирующее устройство (52) вставлено, по меньшей мере, частично в канавку (42), сформированную в участке (34e) сектора (32).5. The ring according to claim 1, characterized in that the damping device (52) is inserted at least partially into the groove (42) formed in the section (34e) of the sector (32). 6. Кольцо по п. 1, отличающееся тем, что демпфирующее устройство (160) охватывает, по меньшей мере, дистальную часть участка (135) крюка опоры (131).6. Ring according to claim 1, characterized in that the damping device (160) covers at least the distal part of the portion (135) of the support hook (131). 7. Кольцо по п. 6, отличающееся тем, что демпфирующее устройство (160) сконфигурировано так, чтобы поддерживать постоянно, во-первых, по меньшей мере, одну зону давления на внешней поверхности участка (135) крюка опоры (131) и зону давления на своей внутренней поверхности и, во-вторых, по меньшей мере, одну зону давления на внутренней поверхности (134i) участка (134) крюка сектора (132) и/или зону давления на внешней поверхности (132e) сектора (132).7. Ring according to claim 6, characterized in that the damping device (160) is configured to constantly maintain, firstly, at least one pressure zone on the outer surface of the support hook section (135) and pressure zone on its inner surface and, secondly, at least one pressure zone on the inner surface (134i) of the sector hook segment (134) of sector (132) and / or the pressure zone on the outer surface (132e) of sector (132). 8. Кольцо по п. 1, отличающееся тем, что демпфирующее устройство (260) охватывает, по меньшей мере, дистальный участок участка (234) крюка сектора (232).8. The ring according to claim 1, characterized in that the damping device (260) covers at least the distal portion of the section (234) of the sector hook (232). 9. Кольцо по п. 1, отличающееся тем, что демпфирующее устройство (54) разделено на множество секций, следующих друг за другом по окружности круга, образованного сектором (секторами) (32), при этом секция предпочтительно соединена с каждым сектором (32).9. The ring according to claim 1, characterized in that the damping device (54) is divided into many sections following each other around the circumference of a circle formed by sector (s) (32), while the section is preferably connected to each sector (32) . 10. Газотурбинный двигатель, содержащий, по меньшей мере, одно кольцо (10) по любому из предшествующих пунктов.10. A gas turbine engine containing at least one ring (10) according to any one of the preceding paragraphs.
RU2015143679A 2013-03-14 2014-03-13 Turbine ring for turbomachine RU2653710C2 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1352257 2013-03-14
FR1352257A FR3003301B1 (en) 2013-03-14 2013-03-14 TURBINE RING FOR TURBOMACHINE
PCT/FR2014/050579 WO2014140493A1 (en) 2013-03-14 2014-03-13 Turbine ring for a turbomachine

Publications (3)

Publication Number Publication Date
RU2015143679A true RU2015143679A (en) 2017-04-26
RU2015143679A3 RU2015143679A3 (en) 2018-03-01
RU2653710C2 RU2653710C2 (en) 2018-05-14

Family

ID=48289407

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2015143679A RU2653710C2 (en) 2013-03-14 2014-03-13 Turbine ring for turbomachine

Country Status (10)

Country Link
US (1) US10138734B2 (en)
EP (1) EP2971609B1 (en)
JP (1) JP6453252B2 (en)
KR (1) KR102199586B1 (en)
CN (1) CN105189937B (en)
CA (1) CA2904951C (en)
FR (1) FR3003301B1 (en)
PL (1) PL2971609T3 (en)
RU (1) RU2653710C2 (en)
WO (1) WO2014140493A1 (en)

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Also Published As

Publication number Publication date
US20160024926A1 (en) 2016-01-28
PL2971609T3 (en) 2019-12-31
US10138734B2 (en) 2018-11-27
RU2015143679A3 (en) 2018-03-01
FR3003301B1 (en) 2018-01-05
KR20150128882A (en) 2015-11-18
RU2653710C2 (en) 2018-05-14
EP2971609B1 (en) 2019-08-07
CA2904951A1 (en) 2014-09-18
CN105189937A (en) 2015-12-23
CN105189937B (en) 2018-03-30
JP2016511362A (en) 2016-04-14
FR3003301A1 (en) 2014-09-19
JP6453252B2 (en) 2019-01-16
CA2904951C (en) 2021-01-26
WO2014140493A1 (en) 2014-09-18
KR102199586B1 (en) 2021-01-07
EP2971609A1 (en) 2016-01-20

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